| タイトル | Figure control of flexible structures - Optical surfaces of thin deformable primary mirrors |
| 著者（英） | Creedon, J. F.; Ostroff, A. J. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1980-12-01 |
| 言語 | eng |
| 内容記述 | Application of a modal control design technique to achieve discrete control of distributed parameter systems is considered. Results are presented for application of the design technique to achieve diffraction limited performance from the primary mirror of a space telescope and to provide flutter suppression for an aircraft wing. |
| NASA分類 | CYBERNETICS |
| レポートNO | 81A14994 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/418700 |
